Thermal analysis and testing of candidate materials for PAIDAE Inflatable aeroshell

20th AIAA Aerodynamic Decelerator Systems Technology Conference

Volumn , Issue , 2009, Pages

  Del Corso, Joseph A ^a   Bruce III, Walter E ^a   Liles, Kaitlin A ^a,b   Hughes, Stephen J ^a,b  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b SED/Structural and Thermal Systems Branch   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC DECELERATORS; AERODYNAMIC LOADING; AEROSHELLS; AEROTHERMAL HEATING; ATMOSPHERIC ENTRY; BALLISTIC COEFFICIENT; BARRIER LAYERS; CANDIDATE MATERIALS; COUPON TESTS; CRITICAL TEMPERATURES; ENTRY VEHICLES; EXPERIMENTAL SETUP; FAILURE CRITERIA; GAS BARRIER; GROUND TESTING; HIGH DENSITY; HIGH HEAT FLUX; HIGH TEMPERATURE; MATERIAL RESPONSE; NASA LANGLEY RESEARCH CENTER; SIMULATION ANALYSIS; SURFACE AREA; TEST SETUPS; THERMAL ANALYSIS; THERMAL PROTECTION SYSTEM; THERMAL SOAK; THREE-LAYER;

AERODYNAMICS; BALLISTICS; HEAT FLUX; HEAT SHIELDING; MATERIALS; NASA; QUALITY ASSURANCE; TEMPERATURE; THERMAL INSULATING MATERIALS; THERMOANALYSIS;

MATERIALS TESTING;

EID: 77958191188     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (5)

1. MSC Patran Users's Manual, MSC Software Corporation, Santa Ana, CA Version 14.0.018, October 4, 2006.
2. Harvin, S.F., Cabell, K.F., Mekkes, G.L., and Gallimore, S.D., "Test Capability Enhancements To The NASA Langley 8-Foot High Temperature Tunnel", JANNAF, 2006.
3. Ferlemann, P.G. "Analysis of the Material Test Sled During Injection into the 8'HTT Test Flow", Technical Note 05-523, TEAMS Contract NNL07AA00B, NASA Langley Research Center, October 29, 2008.
4. Bruce III, Walter E., "Aeroassist Inflatable Reentry System (AIRS) Thermal Protection System (TPS) Thermal Analysis", STSB-2006-002, February 2006.
5. Player, Charles, "PAIDAE Thermal Protection System Testing Final Report - FY2008", PAI-DAE-3.3-012, NASA Langley Research Center, 2008.